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You searched for: subject:"Lift (Aerodynamics"
[texts]Flight investigation at high speeds of flow conditions over an airplane wing as indicated by surface tufts - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613488&ix=nu&I=0&V=D&pm=1
Keywords: Bombers; Lift (Aerodynamics
Downloads: 110
[texts]Effect of trailing-edge extension flaps on propeller characteristics - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003594725&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Lift (Aerodynamics; Aeronautics--Research
Downloads: 111
[texts]Effects of roughness at high Reynolds numbers on the lift and drag characteristics of three thick airfoils - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614465&ix=nu&I=0&V=D&pm=1
Keywords: Reynolds number; Aerofoils; Lift (Aerodynamics; Aerodynamics--Research
Downloads: 186
[texts]Manpower planning models. II, Cross sectional models - Grinold, Richard C.;Marshall, Kneale T.
Title from cover
Keywords: LIFT (AERODYNAMICS); AIRPLANES--WINGS--MATHEMATICAL MODELS
Downloads: 59
[texts]Analysis of factors affecting net lift increment attainable with trailing-edge split flaps on tailless airplanes - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804825&ix=nu&I=0&V=D&pm=1
Keywords: Aeronautics--Research; Airplanes, Tailless; Lift (Aerodynamics; Trailing edge flaps--Aerodynamics
Downloads: 101
[texts]Aerodynamic characteristics of the NACA 747A315 and 747A415 airfoils from tests in the NACA two-dimensional low-turbulence pressure tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638506%26ix=nu%26I=0%26V=D%26pm=1
Keywords: Mach number; Aerofoils; Drag (Aerodynamics; Lift (Aerodynamics; Aerodynamics--Research; Aerodynamics--Research
Downloads: 582
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